WO2021092274A1 - Convertisseur d'énergie électromagnétique - Google Patents

Convertisseur d'énergie électromagnétique Download PDF

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Publication number
WO2021092274A1
WO2021092274A1 PCT/US2020/059262 US2020059262W WO2021092274A1 WO 2021092274 A1 WO2021092274 A1 WO 2021092274A1 US 2020059262 W US2020059262 W US 2020059262W WO 2021092274 A1 WO2021092274 A1 WO 2021092274A1
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Prior art keywords
electromagnetic
energy
cells
cell
power
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PCT/US2020/059262
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English (en)
Inventor
Mojtaba AKHAVAN-TAFTI
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The Regents Of The University Of Michigan
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Priority to EP20884793.9A priority Critical patent/EP4055706A4/fr
Priority to CN202090001063.8U priority patent/CN219018709U/zh
Publication of WO2021092274A1 publication Critical patent/WO2021092274A1/fr

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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/042—PV modules or arrays of single PV cells
    • H01L31/048—Encapsulation of modules
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B64U50/34—In-flight charging
    • B64U50/35—In-flight charging by wireless transmission, e.g. by induction
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/02—Details
    • H01L31/0216—Coatings
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/02—Details
    • H01L31/0232—Optical elements or arrangements associated with the device
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/042—PV modules or arrays of single PV cells
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/042—PV modules or arrays of single PV cells
    • H01L31/05—Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells
    • H01L31/0504—Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells specially adapted for series or parallel connection of solar cells in a module
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/054—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/054—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
    • H01L31/0543—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means comprising light concentrating means of the refractive type, e.g. lenses
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/054—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
    • H01L31/0547—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means comprising light concentrating means of the reflecting type, e.g. parabolic mirrors, concentrators using total internal reflection
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/054—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
    • H01L31/055—Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means where light is absorbed and re-emitted at a different wavelength by the optical element directly associated or integrated with the PV cell, e.g. by using luminescent material, fluorescent concentrators or up-conversion arrangements
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S10/00—PV power plants; Combinations of PV energy systems with other systems for the generation of electric power
    • H02S10/40—Mobile PV generator systems
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S20/00—Supporting structures for PV modules
    • H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S40/00—Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
    • H02S40/20—Optical components
    • H02S40/22—Light-reflecting or light-concentrating means
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S40/00—Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
    • H02S40/40—Thermal components
    • H02S40/42—Cooling means
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S40/00—Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
    • H02S40/40—Thermal components
    • H02S40/42—Cooling means
    • H02S40/425—Cooling means using a gaseous or a liquid coolant, e.g. air flow ventilation, water circulation
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/50—Photovoltaic [PV] energy
    • Y02E10/52—PV systems with concentrators

Definitions

  • the present disclosure relates to a device and method to improve energy conversion to power mobile or stationary devices.
  • Photovoltaic solar panels are commonly used for conversion of light energy into electricity for mobile objects may it be ground-based or air/space-based.
  • Electromagnetic (EM) energy is widely used for powering and propelling satellites (i.e. solar sail).
  • Laser power beaming uses a laser to deliver concentrated light to a remote receiver.
  • the receiver then converts the light to electricity, much like solar powered photovoltaic (PV) cells convert sunlight into electricity.
  • PV photovoltaic
  • laser can be much more intense than the sun
  • laser light can be directed to any place using adaptive optics
  • laser can operate continuously and/or controlled pulses
  • photovoltaics can be optimized to operate with monochromatic laser emission.
  • Power beaming technologies receive energy from a transmitter.
  • the transmitter power is supplied from an electrical outlet, generator, a light concentrator, and/or a power storage unit (e.g. , batteries and fuel cells).
  • the wavelength and the shape of the beam are defined by a set of optics. This light then propagates through air, the vacuum of space, and/or through fiber optic cable until it reaches the receiver. The receiver then converts the light back into electricity/heat/etc.
  • Wireless power delivery requires physical installations at only the transmitting and receiving points, therefore, lowering the cost while enhancing the reliability of the system. Consequently, laser power beaming has numerous advantages over solar power.
  • the present teachings provide a device that is more efficient (power per surface area), less expensive, compact, lightweight, portable, advanced (uses the state-of-the-art technologies to increase efficiency, lower the size and weight of machines by replacing traditional energy storage/delivery by wireless compact devices), etc. than traditional converters.
  • electromagnetic energy converter and method of the present teachings aim to assemble together the existing, well-researched building blocks to enable a more affordable, more efficient and sustainable solution to the energy conversion/harvest problem.
  • the present teachings also provide methods for fabricating multi dimensional solar structures that can be easily manufactured using off-the-shelf solar cells and cheap casting materials such as epoxy resin.
  • the resulting solar structures are found to generate several times the power output of conventional solar panels per occupied surface area.
  • the ease of manufacturing and compact nature of these structures make them particularly attractive for urban settings where available surface areas to mount large solar structures are limited and, therefore, expensive.
  • We also find that the weight and the aerodynamics of these multi-dimensional solar structures can be modified for transportation applications. Presently, bulky conventional solar panels are rarely used aboard mobile vehicles.
  • FIG. 1 illustrates a perspective view of an enclosed electromagnetic (EM) energy converter according to the principles of the present teachings.
  • FIG. 2 is a schematic view illustrating the principles of operation of the present teachings.
  • FIG. 3 illustrates a perspective view of an open-face electromagnetic (EM) energy converter according to the principles of the present teachings having a liquid or solid converter.
  • EM electromagnetic
  • FIG. 4 illustrates a perspective view of an electromagnetic (EM) energy converter according to the principles of the present teachings having a matrix of electric poles that conducts converted EM energy.
  • EM electromagnetic
  • FIG. 5 illustrates a perspective view of the electromagnetic (EM) energy converter of FIG. 4.
  • FIG. 6 illustrates a perspective view of a pair of electromagnetic (EM) energy converters coupled in series according to the principles of the present teachings.
  • FIG. 7A illustrates a perspective view of a plurality of electromagnetic (EM) energy converter coupled in parallel according to the principles of the present teachings.
  • FIG. 7B illustrates a perspective view of an electromagnetic (EM) energy converter mounted around a fiber optic transmitting EM energy and information.
  • EM electromagnetic
  • FIG. 8 illustrates a perspective view of an electromagnetic (EM) energy converter mounted to an EM receiver dish according to the principles of the present teachings.
  • EM electromagnetic
  • FIG. 9 illustrates a second perspective view of the electromagnetic (EM) energy converter of FIG. 8 mounted to the EM receiver dish according to the principles of the present teachings.
  • FIG. 10 illustrates a perspective view of an electromagnetic (EM) energy converter mounted to an EM receiver dish according to the principles of the present teachings.
  • FIG. 11 illustrates a second perspective view of the electromagnetic (EM) energy converter of FIG. 10 mounted to the EM receiver dish according to the principles of the present teachings.
  • EM electromagnetic
  • FIG. 12 illustrates a perspective view of an electromagnetic (EM) energy converter having a roll-able construction according to the principles of the present teachings.
  • EM electromagnetic
  • FIG. 13 illustrates a perspective view of the electromagnetic (EM) energy converter of FIG. 12 having a roll-able construction according to the principles of the present teachings.
  • EM electromagnetic
  • FIG. 14 illustrates a perspective view of an adjustable electromagnetic (EM) energy converter according to the principles of the present teachings.
  • FIG. 15 illustrates a perspective view of the adjustable electromagnetic (EM) energy converter of FIG. 14 according to the principles of the present teachings.
  • FIG. 16 illustrates a perspective view of an electromagnetic (EM) energy converter mounted to an unmanned aerial vehicle (UAV) according to the principles of the present teachings.
  • EM electromagnetic
  • UAV unmanned aerial vehicle
  • FIG. 17 illustrates a perspective view of an electromagnetic (EM) energy converter of FIG. 16 mounted to an unmanned aerial vehicle (UAV) according to the principles of the present teachings.
  • EM electromagnetic
  • UAV unmanned aerial vehicle
  • FIG. 18 illustrates a perspective view of an electromagnetic (EM) energy converter and the principles of operation of the present teachings.
  • EM electromagnetic
  • FIG. 19A is an NREL PV system cost benchmark summary (inflation adjusted), 2010-2018.
  • FIG. 19B is a modeled trend of soft cost as a proportion of total cost by sector, 2010-2018.
  • FIG. 20 is the circuit diagram for Experiment 1 .
  • the solar cell is represented by a diode and two voltmeters measure across the resistor in parallel.
  • the two voltmeters represent that Ni USB 6009 and a handheld digital voltmeter.
  • FIG. 22 shows the automatic output measurements graphed as voltage vs. power.
  • FIG. 23 is the circuit diagram for Experiment 2.
  • FIG. 24 is the solar panel behavior and various light intensities.
  • FIG. 25 is the maximum power point analysis for various light intensities. The points on the graph were created by multiplying the current and voltage ordered pair to get power and then graphed against voltage.
  • FIG. 26 is a cell holder with a PV cell with a diffuser over the cell.
  • FIG. 27 is Voltage vs. Power Output colored by degrees away from normal light.
  • FIG. 28 shows Power Output by degrees from normal light. This test was with no diffuser to determine how power changes by changing angle.
  • FIG. 29 shows Power Output by degrees from normal light. This test was with a 42.8% transparent diffuser to see how changing the power is affected by transparency of the diffuser. This is the diffuser with the lowest transparency that was tested.
  • FIG. 30 shows the characteristic curves of different colored LEDs on a PV cell at 425 (x100 lux).
  • FIG. 31 shows maximum power point analysis for various light sources. The points on the graph were created by multiplying the current and voltage ordered pair to get power and then graphed against voltage.
  • FIG. 32A provides a schematic for three parameters: layers’ angles from incoming electromagnetic radiation Q, layers’ relative angle a, and layers’ relative distance D.
  • the layers A and B are selected from a list consisting at least of photovoltaic cells and optical layers such as mirrors.
  • FIG. 32B is the setup for the plural PV cell tests.
  • FIG. 33 shows voltage vs. power for one and two PV cells.
  • FIG. 34 is the power per surface area exposed to the LED for one PV cell in the dual PV setup. The power per surface area is for each cell.
  • FIG. 35 shows power per surface area exposed to the LED for one PV cell divided by the power per surface area of a single, flat PV cell.
  • FIG. 36 shows the zenith angle vs. power for the two PV cell setup. This test had no reflective material over any of the cells. The points are colored blue if the ratio of 2 cell power over 1 cell power is greater than 2 and red if it is less than 2.
  • FIG. 37 shows the zenith angle vs. power for the two PV cell setup. Each power per area measurement is of a single cell in the two cell setup. The points are colored blue if the performance of a single cell in the two cell test is greater than the performance if the single cell test.
  • FIG. 38 is the setup of the resin tests. The power is measured across both PV cells for each test.
  • FIG. 39 shows the normalized power per area for a flat, single cell in the resin cell setup. This test has no resin in the container.
  • FIG. 40 shows the normalized power per area for a flat, single cell in the resin cell in the resin cell setup with foil. This test has no resin in the container and the container in covered in reflective aluminum foil.
  • FIG. 41 is the normalized power per area (PPA) for 1000 ml_ Clear Resin.
  • FIG. 42 is the normalized power per area (PPA) for 1000 ml_ Clear Resin and foil.
  • FIG. 43 shows the normalized output power of the three tests added together, i.e. , cumulative power per area (PPA).
  • FIG. 44 shows the individual normalized output power percent for each layer in the resin bath at 60 degrees.
  • the line shows the cumulative sum of power for all three layers, i.e., cumulative power per area (PPA).
  • PPA cumulative power per area
  • FIG. 45 shows a schematic of three layers (Layer A, B, and C) selected from a list of PV cells, dielectric material, and reflective material.
  • the layers can be separated by a spacing d to allow for the propagation of electromagnetic energy between layers.
  • the layers are disposed in a medium.
  • the internal surface of the EMEC is coated by a reflective material.
  • FIG. 46 shows a schematic view of an EMEC wherein the transparent body is a dispersive material whose diffusivity varies distally along the structure.
  • the diffusivity gradient can be adjusted to insure that the PV cells, denoted as Layer A and Layer B, generate similar power output.
  • Similar output cells can be connected in parallel or in series for reduced power waste and reduced cost of electronics to harvest the cells.
  • FIG. 47 provides a schematic view of two layers, PV cell, reflective sheet, etc. stacked in a transparent body of diffusive material, the layers labelled Layer A and Layer B.
  • Spacers and/or fillers shown as starts, can serve three immediate purposes: 1 ) to fill the medium to reduce the amount of diffusive material needed to reduce weight and/or cost, 2) to use as spacers such that they hold the layers at a constant distance from each other, and 3) to serve as diffusive and/or reflective surfaces.
  • the spacers can be rods, sheets, or particles. They can be composed of dielectric or conductive materials.
  • FIG. 48 shows a schematic consisting of three PV layers, Layer A, B, and C.
  • the layers are disposed in a transparent medium.
  • the housing encasing the layers and the medium, labelled as External Layer, is either reflective to trap the electromagnetic energy inside the EMEC until it is converted and/or a diffusive layer to disperse the incoming electromagnetic energy for a diffused radiation and to avoid shading across the EMEC.
  • the reflectors can be a combination of surfaces, as shown with black triangles positioned from the layers at distance a, to control the propagation of electromagnetic radiation inside the EMEC.
  • the Layers A and B are separated and/or filled with a layer, shown in grey shading, with a layer of thickness d whose distal cross section is at an angle with the propagating electromagnetic radiation.
  • the layer serves to bring the radiation into the void between Layers A and B until it is converted.
  • FIG. 49 shows a schematic consisting of three PV layers, Layer A, B, and C.
  • An optical surface i.e. , a semi-reflective mirror, a lens, or a wave guide, is positioned at angle with respect to the propagating electromagnetic radiation.
  • the optical surface deflects a fraction of the incoming electromagnetic radiation toward the space between PV cells Layer A and Layer B to convert to electricity.
  • the remaining fraction of the electromagnetic radiation propagates through the optical surface.
  • the optical surface can be processed after the EMEC production, such as bubblegram methods.
  • FIG. 50 shows a schematic consisting of four layers, shown as white rectangles, separated by diffusive layers, shown as grey shaded rectangles.
  • the diffusive layers serve to also guide the incoming electromagnetic radiation toward in between the white layers.
  • FIG. 51 shows a schematic consisting of three layers, Layer A is a PV cell, Layer B is a reflective surface, and Layer C is a PV cell.
  • Layers A and C are transparent and/or diffusive photovoltaics.
  • the gradient grey material illustrates a body of, in this case, 5 layers of transparent diffusive material of different refractive indices to guide the incoming electromagnetic radiation, as shown with bending arrows, toward the spacing between the Layers A and B.
  • Individual layers can be addressed using a matrix of wave guides that direct the incoming electromagnetic radiation independently.
  • the different wave guides are fiber optics, while in other embodiments, the wave guides are covered with reflective material to avoid cross-propagation.
  • the transparent material layer is an Indium tin oxide (ITO) coated glass, where the glass serves to guide and/or diffuse light, while the conductive material, in this case ITO, serves to conduct electricity and/or heat.
  • ITO Indium tin oxide
  • FIG. 52 shows a schematic consisting of three PV layers, Layer A, B, and C disposed fully in a transparent body of material, labelled as ‘Medium’.
  • the medium is circulated inside the EMEC and is extracted to cool and/or heat in a heat transfer system, depicted as a coil encased in a radiating array to conduct heat between the medium and the ambient environment.
  • the heat transfer system may be packaged with the EMEC or coupled as an independent device.
  • the EMEC structure floats above water while the water is further used to cool the system.
  • the temperature regulation is done using a geothermal method.
  • FIG. 53 shows a schematic consisting of four PV layers, Layer A and and C disposed fully in a transparent body of material, labelled as ‘Medium’.
  • Layers A and C are positioned back to back.
  • a layer, Labelled as Layer B such as a pipe, a sheet or a heat coil.
  • Layers B are filled with heat transferring liquid and/or pressurized vapor, shown in solid grey.
  • the purpose of these layers is to transfer the heat associated with the energy conversion process and/or to regulate the temperature of Layers A and C for optimum performance efficiency.
  • the heat transfer is active and is done with the help of a pump, motor, and/or an air compressor, as shown with the grey circle.
  • FIG. 54 shows a schematic view of an example application of the EMEC.
  • the UAV carries an onboard EMEC, consists of a plurality of PV cells disposed in a diffusive, transparent body of insulating material.
  • the EMEC is enclosed within a reflective housing which further encloses the onboard power storage and control systems.
  • the EMEC is, in some embodiments, power by the solar radiation from above where the dome-like lens serves to concentrates the incoming light and to enhance the angle at which the light comes in, in this case, spanning ⁇ 90 degree from the UAV’s axis of symmetry.
  • the UAV can be further powered by a concentrated source of electromagnetic radiation from below, such as monochromatic laser light, concentrated solar radiation, or medium-cross section (e.g., 5-inch) polychromatic light beam, such as a focused flash light.
  • a concentrated source of electromagnetic radiation from below such as monochromatic laser light, concentrated solar radiation, or medium-cross section (e.g., 5-inch) polychromatic light beam, such as a focused flash light.
  • FIG. 55 shows a schematic view of an example application of the EMEC.
  • the compact EMEC which consists of a plurality of PV cells disposed in a diffusive, transparent body of insulating material is installed on an orchard between plants.
  • the co- habitability enables saving on the soft costs associated with dedicating large pieces of land, i.e. , real estate, to conventional solar panels, solely.
  • FIG. 56 shows a schematic view of an example application of the EMEC.
  • the compact EMEC which consists of a plurality of PV cells disposed in a diffusive, transparent body of insulating material is installed beneath the farming grounds and/or in an apartment basement in an urban setting.
  • the EMEC medium extends above ground to collect light.
  • a wave guide is used to collect and bring in light from above the ground and/or an apartment rooftop.
  • the EMEC structures may also contain power storage and control systems onboard or can be connected to other neighboring EMEC structures and to a local power grid.
  • the wave guide can also serve as a shade for plants or a greenhouse.
  • the EMEC structure is under water which can further help with cooling the structure.
  • the heat transfer is radiative, such as in space applications.
  • FIG. 57 shows a schematic view of an example application of the EMEC.
  • the compact EMEC which consists of a plurality of PV cells disposed in a diffusive, transparent body of insulating material is installed above a light post.
  • the EMEC converts ambient light, such as solar radiation in an outdoor setting, into electricity.
  • the electricity can be stored by charging onboard power storage and control systems.
  • the converted light can also be used to power an onboard lighting system.
  • the plurality of PV cells are oriented at similar angles from each other, such as the configuration shown in the drawing.
  • the PV cells are positioned such that the opening cross section is identical between cells to insure that all cells receive the same amount of light and, therefore, generate similar power outputs. This will allow for simple electrical circuits and help to reduce manufacturing and maintenance costs.
  • FIG. 58 shows a schematic view of an example application of the EMEC.
  • the EMEC structures are independent devices. Multiple independent EMEC devices can be connected such that an incoming electromagnetic radiation is shared between devices.
  • the transparent medium of the EMEC devices are in contact such that they enable the propagation of the electromagnetic radiation between EMEC devices.
  • the light propagation is improved by the application of a junction material with refractive properties that optimize the crossing of the electromagnetic radiation between different media.
  • the junction/connection between EMEC devices is made by wave guides, such as fiber optics.
  • Table 1 is a normalized power drop as the angle from normal is increased for the polycarbonate film and acrylic diffusers. This table is for 425 lux and shows how the total power of the system drops at different rates for different diffusers — 425 was chosen as a baseline as it is a median value. The standard deviation of the 100% transparency test is 1.017.
  • Table 2 is a normalized power drop as the angle from normal is increased for the polycarbonate diffusers.
  • Table 3 shows normalized power drop relative to no diffuser on the PV cell as the angle from normal is increased for the polycarbonate film and acrylic diffusers. This table is for 425 lux and shows how the total power of the system is influenced by the use of each diffuser. 425 was chosen as a baseline as it is a median value.
  • Table 4 shows normalized power drop relative to no diffuser on the PV cell as the angle from normal is increased for the polycarbonate diffusers.
  • Table 5 shows a normalized power drop as the angle from normal is increased for different LED colors.
  • Table 6 shows a normalized power drop as the angle from normal is increased for different LED colors.
  • Table 7 shows a normalized power drop to a cell with no diffuser as the angle from normal is increased for different LED colors.
  • Table 8 shows a normalized power drop to a cell with no diffuser as the angle from normal is increased for different LED colors.
  • Table 9 is the power ratio between two and once cell setups.
  • the green cells are where 2 cell power (P2) over 1 cell power (P1 ) is greater than 2.
  • Red cells are where P2/P1 is less than 1.
  • Table 10 is a single PV cell in the dual PV configuration with a reflective surface over the other holder.
  • Table 11 is the power ratio between one cell with a reflective surface and one cell setup.
  • Table 12 is the power ratio between two cell with a reflective surface on one cell and two cells with no reflective surfaces.
  • Table 13 is the power ratio between two cell with a reflective surface on one cell and two cells with no reflective surfaces.
  • Table 14 is a plural colored test for 1-Cell Normalized Green LED Test for the single cell measurement divided by the white LED’s power output for each cell in the table.
  • Table 15 is a plural colored test for 1 -Cell Normalized Blue LED Test for the single cell measurement divided by the white LED’s power output for each cell in the table.
  • Table 16 is a plural colored test for 2-Cell Normalized Green LED Test measuring across a single cell normalized to white LED tests under the same conditions as Tables 14 and 15.
  • Table 17 is a plural colored test for 2-Cell Normalized Blue LED Test measuring across a single cell normalized to white LED tests under the same conditions as Tables 14 and 15.
  • Table 18 is a plural colored test made by taking the values from Table 16 over the values from Table 14.
  • Table 19 is a plural colored test made by taking the values from Table 17 over the values from Table 15.
  • Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well- known processes, well-known device structures, and well-known technologies are not described in detail.
  • first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
  • Spatially relative terms such as “inner,” “outer,” “beneath,” “below,” “lower,” “above,” “upper,” and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures.
  • Spatially relative terms may be intended to encompass different orientations of electromagnetic energy converter 14 in use or operation in addition to the orientation depicted in the figures. For example, if electromagnetic energy converter 14 in the figures is turned over, elements described as “below” or “beneath” other elements or features would then be oriented “above” the other elements or features. Thus, the example term “below” can encompass both an orientation of above and below.
  • Electromagnetic energy converter 14 may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.
  • the present teachings provide an electromagnetic energy converter system 10 (see FIGS. 2 and 18) having an energy source 12 and an electromagnetic (EM) energy converter 14 to convert mono and/or polychromatic wave and/or particle energy from energy source 12 to electricity and/or heat in electromagnetic energy converter 14.
  • EM electromagnetic
  • the present teachings incorporate a third dimension to traditional energy conversion devices to increase conversion efficiency (i.e. watts per square meter).
  • energy source 12 can comprise high-power lasers, particle accelerometers, or other synthetic electromagnetic energy sources radiating waves such as but not limited to radio waves, microwaves, infrared emission, visible emission, ultraviolet emission, X-rays, and Gamma rays to illuminate electromagnetic energy converter 14.
  • energy source 12 can be a naturally- occurring source, such as but not limited to the sun, luminescence, thermal radiation, plasma radiation, radioactive radiation, and vibration.
  • energy source 12, in some embodiments is ground-based, air-based, and/or space-based.
  • the electromagnetic energy used in the present teachings can be of various waveforms including but not limited to short pulses, sine waves, modified sine waves, square waves, and arbitrary waves.
  • the electromagnetic energy used in the present teachings is also selected from a list of monochromatic, polychromatic, polar, non-polar, coherent, non coherent, collimated, and divergent waveforms.
  • electromagnetic energy converter 14 comprises an enclosure case or housing 16 having one or more cells 18 (e.g., a photovoltaic cell, a thermophotovoltaic cell, a thermionic converter, a thermoelectric converter, a piezoelectric converter, an electrochemical converter, ora bio-electrochemical converter) disposed at least partially within housing 16.
  • cells 18 can comprise, but not limited to, inorganic cells, organic cells, amorphous cells, polycrystalline cells, monocrystalline cells, organic light emitting diodes (OLEDs), quantum dots, perovskite cells, thermophotovoltaic cells and the like.
  • cells 18 are comprised of materials in gas, liquid, or solid phases or a combination thereof.
  • cells 18 are in the form of films, slabs, sheets, rods, particles, solution, mixture or the like. These substances are used to convert (monochromatic and polychromatic) EM energy to electricity. It should be understood that electromagnetic energy converter 14 can comprise a plurality of cells 18 being of different types or of similar types with different bandwidths or operational and physical characteristics.
  • electromagnetic energy converter 14 can comprise one or more lenses or optical inputs 20 for receiving and manipulating mono and/or polychromatic wave and/or particle energy from energy source 12.
  • housing 16 can be substantially rectangular shaped having opposing end faces 22 and side faces 24.
  • one or both end faces 22 can include one or more lenses 20.
  • lenses or optical inputs 20 are optional in some embodiments and thus wave and/or particles can be introduced in alternative ways, such as but not limited to through holes, or non-transforming mediums (such as non-optical material).
  • electromagnetic energy converter 14 can comprise a plurality of internal layers or materials 26 disposed along one or more (e.g. all) internal surfaces of housing 16 to direct or manipulate the wave or particle energy within the housing 16 to enhance contact with cells 18.
  • electromagnetic energy converter 14 can comprise an internal layer 26 disposed on an interior facing surface of one or more of end faces 22 and side faces 24.
  • internal layer 26 is a diffusive and/or dispersive and/or luminescent medium.
  • internal layer 26 can comprise a diffusive material/composite, such as but not limited to polymers including acrylic resin, polycarbonate, and polymethyl methacrylate, curable polymers, casting polymers, and reinforced polymers.
  • internal layer 26 can comprise a dispersive medium, preferably a transparent matrix into which a dispersing material is placed. Each dispersing medium has distinct dispersive powers and is comprised of dispersive material such as but not limited to small light-scattering particles such as titanium dioxide crystals and metallic mirrors.
  • internal layer 26 can comprise a luminescent material, such as but not limited to inorganic luminescent materials such as quantum dots, light-emitting dopants and organic and fluorescent Dyes. Luminescent materials can be used to convert the incoming wave and/or particle from one type and/or wavelength to one compatible with electromagnetic energy converter 14 and, specifically, cells 18.
  • internal layer 26 can include a combination of transparent, refractive, diffusive, dispersive, and luminescent characteristics.
  • internal layer 26 comprises one or more highly-reflective and/or non absorbing materials to increase conversion efficiency of electromagnetic energy converter 14. It should be understood that electromagnetic energy converter 14 can comprise a plurality of layers or materials 26 being of different types or of similar types with different operational characteristics.
  • electromagnetic energy converter 14 can comprise one or more active, adaptive, and/or optoelectronic optical systems, generally referenced as 30.
  • Such systems can comprise lenses or waveguides 20 and/or additional one or more optical layers 28 disposed within or outside housing 16.
  • optical layer 28 can be disposed between adjacent cells 18 as illustrated in FIG. 1.
  • Optical layer 28 can comprise diffusive and/or dispersive and/or luminescent medium material, such as but not limited to metallic mirrors.
  • optical system 30 is an active system that actively manages transmission and/or reflection of EM wave and/or particle into electromagnetic energy converter 14 and to cells 18.
  • optical system 30 is housed outside the convertor and is comprised of active and/or adaptive optics 46 to prevent deformation due to external influences such as wind, temperature, mechanical stress or to compensate for atmospheric effects.
  • electromagnetic energy converter system 10 is shown having energy source 12 and an electromagnetic (EM) energy converter 14 operably coupled across a medium 100.
  • medium 100 can comprise any medium operable to transmit wave and/or particle energy, such as but not limited to air, gas, liquid, solid, vacuum, fiber optic, and the like.
  • electromagnetic energy converter system 10 can comprise an optional power converter 32 and a power storage system 34.
  • power converter 32 is configured to convert and/or filter wave and/or particle energy to another form, frequency, and/or type. In this way, power converter 32 can be used to specifically convert ultraviolet beam to, for example, visible beam or other useable form.
  • optical filters are used to alter the wave into a uniform waveform such as polar or collimated waveforms.
  • a diffraction medium e.g., diffraction grating or prism
  • shutters control EM radiation intervals for improved safety and also to enable short-duration pulses of EM radiation.
  • power storage 34 can be operably coupled to electromagnetic energy converter 14 to store and/or otherwise manage the use of the produced electricity output from electromagnetic energy converter 14.
  • electromagnetic energy converter 14 and optional power converter 32 and/or power storage 34 can be carried or otherwise supported by a stationary member (i.e.
  • UAV unmanned aerial vehicle
  • FIGS. 16-18 particular application in a UAV is illustrated in FIGS. 16-18.
  • energy source 12 can comprise a power generator 38, an optional power storage system 40, and a power transmitter 42.
  • energy source 12 comprises, but is not limited to, a diffuse laser 12.
  • electromagnetic energy converter system 10 can comprise a gas, liquid or solid electromagnetic energy converter 14 disposed through a part or an entirety of the internal volume of housing 16.
  • gas, liquid or solid electromagnetic energy converter 14 generally fills a remaining volume within housing 16 unoccupied by associated structure.
  • cells 18 can comprise rod-shaped elements to conduct the EM energy converted into electric current, such as but not limited to reflective rod elements.
  • electromagnetic energy converter 14 can comprise a matrix of electric poles that conducts the converted EM energy.
  • An electric circuit such as schematically illustrated in FIG. 2, can comprise diodes, capacitors, and other electric components to regulate, store, and/or consume the EM energy converted into electric current.
  • electromagnetic energy converter system 10 can comprise a plurality of electromagnetic energy converters 14, 14a, ... 14n to enhance the degree to which the EM beam is converted to electricity.
  • electromagnetic energy converters 14, 14a may be coupled in in series (FIG. 6) and/or in parallel (FIG. 7A).
  • electromagnetic energy converters 14, 14a can be operably and physically coupled via an optical interface or waveguide 44 to permit and facilitate the transmission and communication of waves and/or particles between electromagnetic energy converters 14, 14a.
  • optical interface 44 can be part of optical system 30 and can comprise, but is not limited to, a fiber optic cable.
  • electromagnetic energy converters 14, 14n can be arranged such that each of electromagnetic energy converters 14, 14a, 14n is parallel to an adjacent electromagnetic energy converter and each may include an individual lens 20 or a common lens. Moreover, in some embodiments, each electromagnetic energy converter 14, 14a, 14n can remain self-contained, thereby preventing sharing of wave and/or particle input energy, or may permit transmission of wave and/or particle input energy to adjacent converts.
  • electromagnetic energy converter 14 can comprise a combination of cells 18, different concentrations (radial gradient) of EM energy-dispersive material within a light-transmissive medium 26 enclosed within a housing 22, conductive film, reflective surfaces to reflect the EM energy back into the EM energy-dispersive material within a light-transmissive medium.
  • the EM energy transmits into EM energy convertor through a fiber optic 20.
  • the fiber optic can be stripped of its cladding over a distal length. A fraction of the EM energy enters the EM energy converter while scattering and propagating in the radially-gradient EM energy- dispersive medium.
  • the EM energy is reflected off the reflective end faces 22 and side faces 24 back into the dispersive medium.
  • multiple refractive layers with different refraction indexes are used to selectively guide EM-waves.
  • the directionality and intensity distribution of the EM wave entering the EM convertor may be controlled.
  • the remaining fraction of EM energy propagates through the fiber optic out of the EM convertor on the other end.
  • the outgoing fraction of EM wave may be used to communicate information.
  • electromagnetic energy converter 14 can be mounted on or supported by an EM receiver dish 46.
  • EM receiver dish 46 can comprise a dish member 48 for receiving energy transmitted from energy source 12 or other source (i.e. naturally occurring source).
  • dish member 48 is a parabolic dish supporting electromagnetic energy converter 14 via legs 50 configured to focus the received energy directly to an input (e.g. lens 20) of electromagnetic energy converter 14.
  • a single-bounce configuration of EM receiver dish 46 can be used (i.e. energy received is bounced a single time before focused into electromagnetic energy converter 14).
  • EM receiver dish 48 can comprise electromagnetic energy converter 14 mounted behind dish member 48 and a supplemental active and/or adaptive optics 30 such as a concentrator dish 52 supported by legs 50 is used to focus the energy transmitted to electromagnetic energy converter 14 to a through hole 54 formed in dish member 48 coupled to lens 20 of electromagnetic energy converter 14. In this way, energy can be focused, albeit via two bounces, to electromagnetic energy converter 14.
  • electromagnetic energy converter 14 (singly or with EM receiver dish 48) may be mounted, supported, and carried by vehicles, such as UAVs and the like.
  • electromagnetic energy converter system 10 can comprise an accurate and precise tracking and feedback system 62 for high-precision and reliable energy delivery.
  • adaptive optics 30 can be employed to compensate for potential environmental turbulences.
  • electromagnetic energy converter 14 can comprise a ribbon architecture comprising a centrally disposed fiber optic 56 having a ribbon of cells 18’ and conductive material (e.g., film), together with a reflective or diffusive layer 26.
  • electromagnetic energy converter 14 can comprise roll-able sheets including a photovoltaic material, dispersive medium, reflective medium, conductive (and, in some embodiments, dielectric) material, and waveguides (i.e., refractive medium).
  • the EM energy propagates through the waveguide and can be stripped of its cladding over a distal length.
  • the EM energy is introduced into the converter while scattering and propagating in a dispersive medium.
  • the EM beam is reflected off the reflective surfaces.
  • a generally adjustable electromagnetic energy converter 14’ is a function of the relative positions of an array of disks 58 interspersed within cells 18 (disposed in parallel).
  • the output of electromagnetic energy converter 14’ is changed via rotation of disks 58 to obstruct or otherwise reveal cells 18 to incoming EM wave and/or particles.
  • the relative position of the array of disks is changed by rotating a pin member 60 operably coupled to disks 58 that selective, partially, and/or completely obstructs or otherwise reveals cells 18 to EM wave and/or particles entering lens 20.
  • the array of disks 58 is coated with refractive and/or reflective materials.
  • An electromagnetic energy convertor (EMEC) device is optimized via adjusting three main system characteristics: 1 ) number of photovoltaic (PV) cells, 2) relative PV cell angle, 3) medium transparency diffusion coefficients.
  • Other adjustable parameters include: PV cell stacking density, light intensity, light frequency, load resistance, medium dielectric constant (i.e. , refractive index), EMEC weight, and light collection aperture.
  • the PV cell is an off-the-shelf silicon-based material.
  • the PV cell comprises an organic material (e.g., OLED and perovskite material) to convert electromagnetic energy to electrical current.
  • the PV cell is not opaque.
  • the PV cell is coated with a reflective layer to reduce light absorption.
  • the PV cell is specifically selected to operate within a narrow range of wavelengths.
  • the PV cell operates within one (or more) range of EM frequencies.
  • the PV cell is coated in a dielectric material to avoid short-circuit between cell terminals (or discharging).
  • the dielectric-coated PV cell is submerged in a high-specific heat fluid, such as deionized water.
  • the fluid medium circulates and can exchange heat.
  • the medium within which the PV cells are at least partially deposited is a gas mixture.
  • the medium is an insulating material and is a mixture of materials of more than one state of matter.
  • air packets are introduced with in a solid matrix of resin to reduce system weight.
  • a photovoltaic cell is first characterized. The cell is then used in combination with other cells while the 3 main system characteristics are adjusted. The EMEC overall output is compared with a cell of the same occupied surface area. Therefore, relative performance is defined as the ratio of the power output of the EMEC per occupied surface area and the power output of flat cells occupying the same surface area.
  • the USB microcontroller used for the measurement algorithm was the Nl USB-6009.
  • the light source was a Chanzon 100W LED and emitted illuminance from (25 - 775) x 100 lux of natural white (4000 K) light.
  • the Chanzon LED is connected to a DC power source.
  • the power source is controlled by an PC.
  • V1 voltages across a resistor connected in series with the photovoltaic (PV) cell were also measured using a manual voltmeter, V2.
  • the solar cell tests were consistent in automated measurements using the automatic measurement algorithm and manual measurements using a multimeter. The tests were run 3 separate times and averages were calculated for error analysis purposes. Both measurements could not exceed 0.5 V for output voltage because of the characteristics of the solar cell.
  • MPP maximum power point
  • Isc is a characteristic that occurs when there is no voltage drop across the terminals. Isc is important to measure because it tells us the highest current that can flow in the circuit for various light intensities. Taking out the resistor and connecting the panel wires will result in Isc. This is equivalent to having the 0 W resistor. These behaviors of the solar panel will be useful to know for further test.
  • FIG. 24 indicates that the short circuit current of this particular photovoltaic cell will not exceed 200 mA for light intensities less than 775 lux. This can help us categorize the types of equipment to use. If a multimeter cannot take over 200 mA for a certain reading, we know that it will be safe to use for a single cell. The voltage will range from 0.4-0.5 V open circuit and will never pass 0.5 V. This can help us in the same way as the current.
  • FIG. 25 provides a voltage vs. power profile for the particular cell.
  • the profile can help with efficient use of the photovoltaic cell.
  • a single cell can produce around 26 mW.
  • the additional benefit of power generation decreases showing diminishing benefit of each increasing light intensity. This occurs because of the cell’s characteristics of Isc and Voc not allow anymore current, and therefore power generated, after Voc is reached.
  • the maximum power point can be determined for each light intensity to find the resistance that gets closest to that point. Understanding MPP can help with maximizing the efficiency of the system.
  • the thickness of the holder is 4 mm and 1.75 mm where the PV cell sits. Including the thickness of the cell and the glue that sits underneath the cell, the diffuser is around 1 .5-2 mm away from the cell’s surface for these tests.
  • FIG. 27 shows the voltage vs. power graph for the PV cell without a diffuser.
  • the distribution shows that there is a correlation between angle from the light and output voltage.
  • the lower angles have a higher output voltage and create more power and the higher angles have a lower output voltage and create a lower power output. This relationship is true most cases when the light intensity is held constant.
  • This graph shows that power depends on degrees from the light, to go along with the light intensity dependency.
  • the power is nearly zero past 90 degrees for all following degrees.
  • the power is also not as consistent at the top as the power starts to fall down approaching 90 degrees. It is also important to note that the axis for Power is in watts and FIG. 28 is in milliwatts.
  • the diffuser blocks more light from reaching the cell and therefore less power is produced.
  • Table 1 The takeaway of Table 1 is to show the different rates of change in power output for different diffusers. There is no real pattern to the decrease in power output across the range of diffusers. Most diffusers decrease substantially after 90 degrees as seen in FIGS. 26-27, but some diffusers decrease more steadily, like 91.6% and 87.7%. In a couple specific cases, some diffusers actually increase power when they are turned further from the light source. This happens for 91.6% at 110 degrees and 91.5% at 100 degrees. Most of the diffusers increase slightly after the turn from 170 to 180 degrees, when the cell is facing directly away from the light.
  • the rest of the diffusers are made out of acrylic and experience more gradual drops in power output, except for 64.8%. 64.8 is different in color (white) than the other acrylic diffusers and could the reason for sharp drop at 90 degrees.
  • Table 2 is a continuation of Table 1 for the polycarbonate diffusers. All of the polycarbonate diffusers have the same thickness and the same surface texture. The first four (89.1 , 55.6, 53.2, and 52) are considered translucent cool for their color and the rest are translucent warm. The diffusers all drop in power output around 90 degrees. The behavior of the diffusers are more consistent across the table as they are all made of the same material. The polycarbonate diffusers start to become useful at the 90 degree mark, as these diffusers hold their power output better than using no diffuser.
  • Table 3 shows the benefit or harm of using a diffuser at certain angles in terms of total power output. Most of the diffusers increase the power output for angles below 90. The differences in the diffusers really show for angles at or above 90. Some diffusers increase the power output whereas some decrease it. The polycarbonate film diffusers decrease power output after 90 degrees. This tells us that using no diffuser past 90 degrees is better than using a polycarbonate film diffusers. Most acrylic diffusers improve power output past 90 degrees. The diffusers that performed the best, (94.2, KSFI 93, 91.6, and 87.6), are all made out of acrylic.
  • the 87.6 diffuser made out of polycarbonate film, increases the power output at 90 degrees, but then decreases in performance similar to other polycarbonate film diffusers. Again, the transparency is not the only factor in changing the power output. Some more transparent diffusers are outperformed by less transparent diffusers, and some less transparent diffusers are outperformed by more transparent diffusers. Proof of this is in the difference in performance between the two 93% transparent diffusers.
  • Table 4 is a continuation of Table 3 for the polycarbonate diffusers.
  • the polycarbonate diffusers all perform the best after the 90 degree mark. All diffusers except the 52% significantly increase the power of the PV cell at the 90 degree mark to the 110 degree mark.
  • the polycarbonate film diffusers are their most useful in this range and can increase the power output of the cell. These tests will further help maximize power of the EMEC device based on the orientation and angle to the light.
  • the goal of the diffuser experiments is to find the best set of conditions to use the PV cell to maximize power output. These tests can serve as a reference when designing the black-box device. Power decreases as the cell is rotated away from direct sunlight. Certain diffusers can improve the performance of the cell at certain angles. These combinations can be used with diffused light to create more power from PV cells not in direct light.
  • the polycarbonate diffusers can be used at lower incident angles to retain efficiency.
  • Acrylic diffusers should be used at higher incident angles past 90 degrees to optimized cell efficiency.
  • FIG. 12 shows the various characteristic curves for the different colored LEDs.
  • the wavelength of the light appears to have a significant effect on the V_OC and l_SC characteristics of the cell.
  • the colored LEDs bring down both V_OC and l_SC of the cell.
  • the green LEDs pulls the current and voltage down further than the blue. It is also important to note that blue has a shorter wavelength than green in the visible light spectrum.
  • FIG. 31 shows the maximum power for the different LEDs.
  • the white light has the highest potential power output followed by blue light and green light. These results also follow the wavelength pattern of the visible light spectrum.
  • the color of the light is another factor that can be manipulated to achieve desired characteristics of the cell.
  • white light is the best light source for selected PV cell.
  • Tables 5 and 6 shows the benefit or harm of using a diffuser at certain angles in terms of total power output by LED color.
  • the overall power output trend of the diffusers is constant over different colored LEDs.
  • the starting reference power values are all higher for the blue LED.
  • the green LED performs worse at angles past 100 degrees for most diffusers.
  • the 180 degrees values are all under 0.5% for the green and over 0.5% for the blue.
  • Table 5 shows a large difference in power output around the 90 degree mark. All of the diffusers are worse than reference at 80 and 90 degrees for the green light. After 90 degrees, the results are less consistent.
  • the 5 best performing diffusers past 90 degrees for the green LED (KSH 63, 91 .6, 91 .5, 79.1 , and 61 .5) are all made out of acrylic.
  • the worst performers past 90 were made out of polycarbonate film except for 64.8, which is made out of acrylic. 64.8 performed poorly for the white LED test as well, whereas the other acrylic diffusers performed better.
  • Table 6 is for the blue LED tests. The effect on power output is not consistent across all diffusers. There is not a large drop around the 90 degree mark for most of the diffusers. The diffusers that have a transparency in the 90s performed the worst for the blue LED. This was not the case for the green LED, as KSH 93 performed the best out of all the diffusers. Diffusers below the 90% transparency mark increased power output for the most part past 90 degrees.
  • FIG. 32A provides a schematic for three inter-dependent parameters: layers’ angles from the incoming electromagnetic energy Q, layers’ relative angle a, and layers’ relative distance D.
  • the layers A and B are selected from a list consisting at least of PV cells and optical layers such as mirrors.
  • the relative distance D refers to the stacking density of the layers. The relative distance D will determine the light intake cross section of Layer A and Layer B. Smaller D will result in smaller amount of light entering between the two layers.
  • the medium shown in grey, is resin.
  • the resin is liquid in some embodiments, while a solid, i.e. , hardened, in other embodiments.
  • the transparency and the diffusivity of the medium is modified in some embodiments using color pigments, such as dyes, and air bubbles.
  • the resin medium is thinned by adding acetone.
  • the cells were placed in holders connected to 200 step motors.
  • the motors were controlled using an chicken Uno and the chicken IDE and the voltage was measured across a 100 W resistor using the Nl USB-6009.
  • the cells started flush against each other, and were then open in steps of 10.8 degrees from 0-180 degrees. These measurements were picked on the limits of the stepper motors.
  • Each step from the motor is 1.8 degrees and 5 steps gives 9 degrees to try and mimic the single cell test angles.
  • the cells were equidistant from the light source at all times and since both cells are of the same design, we assumed that the potential across each cell was equal.
  • the voltage for the two cell setup is the total voltage, so the voltage of a single cell is the voltage divided by 2, as shown in FIG. 33.
  • the plural cell setup results in doubling the maximum voltage across the resistor. These points occur at the open circuit voltage and is therefore a characteristic of the cell.
  • the voltage almost reaches 1 V for the two cells and the single cell reaches around 0.5 V.
  • the total power of the device is doubled as a result.
  • the overall power distribution of the one cell setup grows twice as fast as the two cell setup.
  • the power per surface area (PPA) for the two cells ranges up to 5 W/m 2 per cell.
  • the angle is taken from normal to receiving light.
  • the points that are almost always paired up are just on either side of normal.
  • FIG. 35 shows the best way to utilize area inside the EMEC to produce the most power. PV cells normal to receiving light produced the most power (FIG. 9).
  • the cells can produce up to 4 times the power per area than a flat cell at 90 degrees from normal (0 or 180 degrees from zenith). Multiple cells should be utilized vertically or close to vertical to maximize power per area.
  • FIG. 36 shows the power output for the two cell setup by angle.
  • the blue points are the points where the interaction of multiple cells is beneficial the blue points are locations in which adding a second PV cell more than doubles the power output.
  • the conditions in which this happens is for high light intensities and small zenith angles. This is a result of the reflection of light between the cells which occurs in a larger amount when they are closer together. The result is less predominate at higher angles because of a larger angle of incidence and the cells are already operating close to their Voc points.
  • Table 9 is the same data as FIG. 35 just listed out in a table.
  • the cells had no reflective material over them and the power ratio is listed in each cell.
  • the conditions where the two cells system receives extra benefit (power more than doubles) from a second cell occurs for small angles. For the medium and higher angles, there is not this extra benefit of adding a second cell.
  • the red cells are where adding a second cell actually decreases performance of the system. This occurs because the cells are connected together. The drop in performance of a single cell in the series will drop the power in other cells in the series.
  • the gain in power output by adding a second PV cell can be seen in FIG. 37. These are the blue points where each cell in the e plural cell setup outperforms a single cell. These locations again occur at small angles, where the cells are the closest to each other. These conditions are where light reflects off the cells into each other and increases power, as seen in FIG. 36.
  • the final zenith angle of 171 has a large drop in power per area compared to the single cell in FIG. 34. This is the first angle that shows a significant decrease in power by adding a second cell. There is less light at 171 degrees and the PV cells are not working efficiently. This hurts the setup as a whole and decreases potential power output from a second cell.
  • Table 12 The purpose of Table 12 is to characterize the reflective surface used in following reflectivity tests.
  • the reflective surface used was 35% tint, silver vinyl surface used for automobile windows.
  • the power of the single cell is boosted at small angles. This is expected as the cells are closest to each other and the chance for reflectivity is the greater.
  • the cell also increases in performance at the 180 degree mark. This reflectivity test for the cell helps understand the impact of using this specific vinyl and the optimal zenith angle and lux combination.
  • Table 11 shows the base effectiveness of using a reflective cover over the cell for a single cell setup. The power decreases for all cases except for zenith angles of 180. The only benefit of using a reflective surface on a single cell in the orientation would be at 180 degrees. The purpose of this test was to characterize how the reflective surface works and the results of using it in power output.
  • Table 12 shows the benefit or hindrance of putting a reflective surface on one cell in the two cell setup.
  • the benefit of the reflective surface only occurs at zenith angles of 171 and 180 degrees. These angles are when the cells are facing directly away from each other. Therefore, there is no light that is being reflected from one cell to the other. The added benefit at these angles have to do with the performance of the reflective vinyl as seen in Table 11 . There is no reflective benefit for small angles, where the cells are closest together and interacting the most.
  • Table 13 compares the power for a two cell setup and a two cell setup with reflective vinyl over both of the cells. The power is reduced in all situations and conditions.
  • the reflective surface does not appear to have increased power substantially for any of the cell layouts. Other reflective materials or other transparencies could be tested to find the best way to utilize the cell with a reflective layer.
  • Experiment 7 shows the effect of using a green and blue LED in the plural PV cell setup in Experiment 6. This test will see how the power is affected by different wavelengths of light and to see how consistent the results are for single cell colorized tests. This characterization will help maximize power output of the cell combination.
  • the cells were tested in the same way as in Experiment 6, from 0-180 degrees using a green LED, blue LED, and white LED.
  • the first test used only one PV cell to create a baseline for the cell in this configuration for different colored LEDs.
  • the second test tested two cells in series with voltage measured across one of the cells. This test also used the three different colored LEDs. Since the white LEDs had the highest power output in Experiment 4, the results of the colored LEDs were compared and normalized to the white light power measurement.
  • the green LED does not have much benefit over the white, as almost all the points result in a number less than 1 , or a decrease in power output.
  • the blue LED can be seen to increase the power output for small angles and could be a result of the absorbance of blue light. Blue light has a low absorbance and has a greater chance of reflecting from cell to cell than white light.
  • the final two tables were made by taking the values from the second set of tables over the values from the first set of tables. These tables show the power output percent increase change from adding a second cell for each LED color. The purpose of these tables is to show how much more blue or green light can be utilized by adding another cell. These result in an increase in performance of a single cell in the setup.
  • Both colors increase in power output by adding a second cell for higher zenith angles. As the angle between the cells increases, a second PV cell in the setup will result in substantially increasing performance of each cell.
  • Experiment 3 showed the benefit of using a solid, diffusive material to scatter light and provide light to the PV cells.
  • Resin is beneficial in the design of EMEC devices as the resin can be easily poured over the cells without worrying about the positioning unlike with solid diffusers.
  • the plural resin tests were ran using varying amounts of clear resin.
  • the resin is a solution of resin and ethanol to lower the viscosity of resin. Resin amounts used were from 0 ml_ to 10OOmL in steps of 200 ml_. Each amount of resin had secondary tests that covered the container in a reflective surface (aluminum foil).
  • the cells started horizontal with a zenith angle of 90 to the light source.
  • the cells were rotated towards each other in steps of 9 degrees until the cells were parallel to each other.
  • the angle measured in the tests was the angle to the horizon of the PV cells (referred to as altitude angle).
  • the power per area numbers were then normalized to the power per area of a flat PV cell with no resin. This normalization shows the benefit of using resin in terms of saving the needed to maximize power from the cells.
  • FIG. 39 shows normalized power per area (PPA) for a base cell in the resin container.
  • the maximum PPA for the PV cell is around 5 W/m 2 when the cell in nearly vertical. This shows similar results to FIG. 16, as the maximum PPA for that uncovered cell was also around 5 W/m 2 .
  • FIG. 40 shows the result of covering the container in aluminum foil. This ensures the container will not absorb any light and deflective it up back towards the cells. This results in the maximum PPA being a little over 5 W/m 2 at 81 degrees from the horizon. The results are not drastically different from FIG. 39 because the cells are facing upward, towards the light. The light reflected by the foil has a small impact on the upward facing cells. Further figures and charts with foil will be normalized to flat cells in the foil setup as there is a small increase in PPA with using foil.
  • FIGS. 41-42 show the PPA for the maximum amount of resin used with and without resin respectively.
  • the foil test shows a small increase in PPA compared to no foil again as seen in earlier tests.
  • the lower lux intensities, such as 25 and 75 lux, show odd behavior compared to the higher intensities. This is a result from the characteristics of the resin used.
  • the resin is not completely transparent and smaller light intensities have a problem reaching the cells for higher angles. At smaller angles, the light is not diffused as well and easily shines on the flat cell.
  • the tests show that a diffusive material, such as resin, can save space when using PV cells, therefore, improving power per unit area significantly.
  • the resin allows for light to be diffused throughout the container and to be shared across cells.
  • the resin also allows for the cells to be positioned in ways such that the PPA can be maximized. Maximizing the PPA will allow for more cells to be used in a smaller area and to allow more power from the same amount of space.
  • Experiment 8 shows the benefit of using resin to maximize the power per area of the solar cell.
  • the resin allows for the soft light to be spread throughout the container, powering multiple cells with necessarily needing direct light.
  • This experiment shows the potential for using multiple layers of PV cells in varying configurations to maximize the PPA of the entire setup. The purpose of this is to create more power using the same amount of land, resulting in more efficient power production.
  • the first test set the PV cells in the same way as in Experiment 12. The cells were facing upwards and rotated in 9 degree intervals.
  • the second test placed the cells on the bottom side of these holders. The light was reflected off the container and reached the upside down cells from the bottom.
  • the third test placed two cells at the bottom of the container with the resin over them. The cell holders were in the same position as the first two tests and rotated in the same manner. The purpose of the holders was to block the light where the face up and face down cells would be.
  • FIG. 43 shows the PPA percentage compared to a flat cell being at 100%. This figure shows that the light can be used to power three different layers of cells to increase the PPA of a cell up to 11 times at higher angles. Even at small angles, using layered cells shows an increase in power produced. This graph shows that the stacking of cells is beneficial in any scenario when using resin.
  • FIG. 45 shows schematic of three layers (Layer A, B, and C) selected from a list of PV cells, dielectric material, and reflective material.
  • Layers A, B, and C are PV cells, wherein Layers A and Layer B face each other. Layers B and C are positioned facing away from each other.
  • the spacing between layers A and B is d to allow light to propagate between them.
  • the ratio of spacing, d, and total light intake cross section inside the EMEC, a can be optimized.
  • the layers are disposed in a medium.
  • the medium can change radially and/or distally inside the EMEC.
  • Some of the properties of the medium include transparency, diffusivity, specific heat, viscosity, freezing point, boiling point, and, absorption. The transparency is within a range 0 to 1 , where 0 means no transmission.
  • medium properties are a function of electromagnetic radiation wavelength.
  • the medium is doped with spacers, marked as stars, whose goal is at least one of the following: 1 ) to reduce the total weight, 2) to determine the spacing d, and 3) to diffuse the electromagnetic radiation.
  • the spacers are air bubbles.
  • the spacers are clear plastic pellets of (known) uniform diameter.
  • the medium is a flexible material such as silicon or a gel. In other embodiments, the medium consists of inflexible materials once hardened.
  • the internal surface of the EMEC is coated by a reflective material, as illustrated by black triangles in FIG. 48.
  • the spacing between neighboring PV cells (Layers A & B) is filled with a waveguide of thickness d.
  • the waveguide intake light cross section is intended to capture light with cross section a, propagating in both directions (top to bottom and bottom to top) in the medium.
  • reflective and or diffusive surfaces are positioned near the spacing between neighboring PV cells (Layers A and B) whose purpose is to reflect at least a fraction of the propagating light. The reflected and/or diffused light will then propagate between Layers A and B and is converted to electricity.
  • the reflective surface is a mirror.
  • One example of the diffusive surface is an etching inside the medium.
  • the etching can be created after the hardening of the medium (e.g., epoxy resin + hardener) using laser bubblegram fabrication techniques.
  • a bubblegram also known as laser crystal, 3D crystal engraving or vitrography
  • the medium at least partially changes properties.
  • the medium includes layers of reflective liquid crystal surfaces whose macroscopic properties can be changed under various electric or magnetic perturbations.
  • the medium can change phase, for instance, from liquid to solid and back to liquid again. For instance, a water-based medium can be cooled to below freezing point temporarily for different dielectric properties.
  • the spacing between Layers A and B can also be filled with diffusing waveguides, as depicted in FIG. 50.
  • the diffusing waveguide scatters the incoming electromagnetic radiation. Some of the scattered electromagnetic radiation is then propagated within the waveguide and converted to electricity by Layers A and B.
  • the medium is divided between distally- and radially-varying dielectric material of differing refractive indices, as shown in FIG. 51.
  • the purpose of such waveguide with gradient refractive index profile is to address individual PV cell spacings.
  • the medium is a waveguide matrix within which light propoxates along an intended path.
  • the purpose of the varying refractive indices is to direct the light by bending it at the interface of neighboring dielectric materials of varying refractive indices.
  • the medium is of liquid phase and can be circulated.
  • Some of the advantages to liquid medium include: 1 ) heat dissipation, 2) medium replacement, and 3) PV cell replacement.
  • the medium is circulated between the EMEC enclosure and a piping system in order to transfer heat from inside the enclosure and discharging it to the surrounding air (or other surrounding media).
  • Other methods of heat transfer include: convection, conduction, thermal radiation, and evaporative cooling.
  • the PV cells of the EMEC are coated with dielectric insulating material and submerged in a polar liquid such as deionized water with relatively high specific heat.
  • the EMEC’s transparent insulating body consists of a circulatable polar liquid and the insulating dielectric material.
  • the liquid is conductive and polar such as water
  • the liquid medium is an insulator, such as epoxy resin.
  • the EMEC medium is a diffusive gas, such as smoke and water vapor, which can be circulated for heat transfer.
  • the cooling mechanism involves circulating an evacuated tube of clear or reflective surface partially filled with a fluid such as alcohol or water. Due to the low pressure, the fluid inside the pipe may boil when it absorbs heat from the air inside the EMEC enclosure. The fluid and/or vapor circulates through the pipe between the PV cells inside the tube. Once outside the EMEC enclosure, the fluid (and/or vapor) is cooled by the air outside the enclosure (and condenses). The (condensed) fluid then returns to the bottom of the enclosure and the cycle repeats.
  • the heat transfer process is active using an air compressor or a fluid circulator pump.
  • the heat transfer system includes a temperature regulator whose purpose is to regulate the temperature of the PV cells and/or the medium for optimized PV cells power output. This embodiment aims to provide the appropriate temperature for the PV cells whose efficiency is a function of ambient temperature. In some other embodiments, the PV cell and/or the medium temperature is kept at sub-zero degrees Celsius for optimized power output.
  • the EMEC is fabricated layer by layer.
  • fabrication process include: 3D printing, chemical vapor deposition, roll-to-roll fabrication, laser etching, and chemical curing such as thermosetting and radiation setting.
  • the electromagnetic energy intake cross section is modified to enhance or reduce the amount of incoming energy.
  • the aperture setting is done using active components such as mechanical gates.
  • the energy intake is controlled with a layer of liquid crystal.
  • electromagnetic energy converter system 10 and/or electromagnetic energy converter 14 has been disclosed that is particularly suited for use in any one or a number of applications, including, but not limited to, the efficient delivery and/or storage of transmitted power.
  • electromagnetic energy converter system 10 and/or electromagnetic energy converter 14 can be used, for example, to power compact solar structures, microelectromechanical devices (MEMS), electronic circuits and devices, transportation elements (e.g. buses, trains, cars, aircraft, and the like), space and long distance applications (e.g. satellites in orbit or aircraft in general (airplanes, UAVs, etc.)).
  • MEMS microelectromechanical devices
  • transportation elements e.g. buses, trains, cars, aircraft, and the like
  • space and long distance applications e.g. satellites in orbit or aircraft in general (airplanes, UAVs, etc.
  • the principles of the present teachings replace bulky and fragile solar panels with a reliable, resilient, compact, lightweight device that is mobile and efficient.
  • the EMEC can be implemented into the design of transportation devices such as a UAV.
  • the EMEC will convert incoming radiation (solar radiation and/or concentrated source of electromagnetic energy, such as a laser) into electricity which can be stored and consumed aboard.
  • the EMEC devices can be designed with optimized aerodynamics and can be installed aboard vehicles, such as trucks and vessles.
  • Farms unlike traditional solar farms which occupy vast surface areas to generate power, the compact EMEC, as shown in FIG. 55, can be implanted on farms, between crops, to convert solar radiation to electricity.
  • the electrical power can be stored and consumed onboard, for example for lighting, and or transferred to the power grid.
  • EMEC devices can be used to harvest electricity. Solar radiation can be collected and directed into an EMEC enclosure by a waveguide.
  • the EMEC enclosure and electronics are installed underground.
  • Another benefit of underground EMEC installations is thermal management.
  • the relatively-constant soil temperature, specially at depths greater than 30 ft, can be used to regulate the EMEC temperature.
  • the EMEC is used to convert solar radiation to electricity to power urban lighting structures, such as light posts, as shown in FIG. 57.
  • multiple EMEC devices can be coupled together. Two important advantages of this design are: 1) easy installation, and 2) easy maintenance.
  • the EMEC devices are wrapped around an existing light post.
  • the junction between neighboring EMEC devices is filled with a junction material to manage the propagation of light between EMECs. Faulty EMECs can be easily replaced.
  • T ransparent material a transparent material refers to a type of material that transmits at least in part of the electromagnetic energy spectrum. Transparency can range between 0 (no transmission) and 1 (100% transmission). The non-transmitted electromagnetic energy can be absorbed by the material and/or deflected.
  • Diffusivity materials with optical diffusivity diffuse or scatter electromagnetic radiation with or without absorption. Repeated scattering of the electromagnetic radiation can change its direction, often referred to as ‘random walk’.
  • Diffusive material can further be diffractive, also known as ‘diffractive diffuser or homogenizer’ to diffract (and refract) an incoming monochromatic electromagnetic radiation for a particular spatial configuration and/or intensity profile. Diffusivity can range between 0 (no scattering) and 1 (complete reflection and or absorption).
  • Insulating material an insulating material is a dielectric material with known dielectric constant and refractive index (i.e. , finite real and imaginary dielectric constant). In some embodiments, the insulating material may also serve as a thermal insulator to reduce heat transfer between the EMEC medium and the surrounding environment.
  • the insulating material insulates the PV cells from moisture and other conductive and/or oxidizing agents.
  • electromagnetic (EM) energy converting cells comprise of a photoelectric layer that converts electromagnetic energy to electricity. This layer can be made of a material selected from a list of conductors (e.g., copper), semi-conductors (e.g., silicon crystals and quantum dots), inorganic materials, and organic materials (e.g., perovskite and organic light emitting diodes).
  • the electric current generated in the photoelectric layer of the electromagnetic (EM) energy converting cell is transferred by conductive poles/terminals.
  • the term ‘plurality’ refers to more than one electromagnetic (EM) energy converting cell.
  • the excluded structure describes a traditional solar panel wherein all PV cells are oriented facing up and positioned in a single plane.
  • the plurality of electromagnetic (EM) energy converting cells can be electrically coupled. In some embodiments, the coupling between the electromagnetic (EM) energy converting cells is done in a series configuration. In other embodiments, the electromagnetic (EM) energy converting cells are connected in a parallel configuration.
  • the electromagnetic (EM) energy converting cells are individually addressed (harvested), while in other embodiments, the cells are addressed as a group wherein the electrical charge from a plurality of cells of similar power output are connected and harvested.
  • Single-Piece encapsulating material the term ‘encapsulating’ means to at least partially enclose the electromagnetic (EM) energy converting cell of the EMEC in an insulating material.
  • Single piece refers to a material or a plurality of materials that can transmit at least some electromagnetic energy wavelengths.
  • the single-piece insulating material holds the electromagnetic (EM) energy converting cells of the EMEC in position, such as a hardened epoxy resin, while in other embodiments, as described above, the single-piece insulating material consists of a dielectric material to cover the electromagnetic (EM) energy converting cells while the covered cells are immersed in a diffusive and/or heat-transferring liquid material.
  • EM electromagnetic
  • One common characteristic between the aforementioned single piece encapsulating materials is that they all serve as a medium within which electromagnetic energy is transmitted until converted to electricity by the plurality of electromagnetic (EM) energy converting cells.
  • Another common characteristic of the single-piece encapsulating materials is that they all prevent the flow of electric current between the positive and negative terminals of electromagnetic (EM) energy converting cells, i.e.
  • the single-piece encapsulating materials are at least partially electrical insulators within which electric charges do not flow freely, even under the influence of an electric field, i.e., potential difference across the terminals.
  • Power per surface area refers to the amount of electrical power generated over the footprint, i.e., the occupied surface area by an EMEC.
  • the normalized power per surface area is the ratio of EMEC power per surface area and the power output of flat cells occupying the same surface area as the footprint of the EMEC, i.e., (P/A)EMEC / (P/A)fiat DCis, under similar electromagnetic radiation and environmental conditions.

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Abstract

L'invention concerne un système multidimensionnel fermé destiné à convertir de l'énergie électromagnétique (EM) en électricité. Un dispositif de convertisseur d'énergie électromagnétique (EMEC) comprend une pluralité de cellules de conversion d'énergie électromagnétique (EM) disposées en une seule pièce, au moins partiellement transparentes, un milieu isolant choisi parmi une liste de matériaux luminescents, transmissifs, absorbants, diffusifs, réfractifs, dispersifs, conducteurs et diélectriques ou une combinaison de ceux-ci. Le milieu facilite la propagation de l'énergie électromagnétique à l'intérieur du dispositif EMEC et aide à optimiser sa conversion en électricité par la pluralité de cellules de conversion d'énergie électromagnétique (EM). La pluralité de cellules de conversion d'énergie électromagnétique (EM) sont disposées au moins partiellement à l'intérieur du milieu. L'invention concerne également un procédé d'optimisation de la puissance par zone de surface occupée du dispositif de convertisseur d'énergie électromagnétique (EMEC) par réglage de la diffusivité du milieu et des positions de réglage et/ou des orientations de la pluralité de cellules de conversion d'énergie électromagnétique (EM) par réglage d'au moins l'un de trois paramètres physiques principaux.
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US20200119684A1 (en) 2020-04-16
US20210075361A1 (en) 2021-03-11
US11935978B2 (en) 2024-03-19
WO2019051178A1 (fr) 2019-03-14
EP4055706A1 (fr) 2022-09-14
DE112018004929T5 (de) 2020-06-18

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